I.Ae.32 Chingolo
| I.Ae.32 Chingolo | |
|---|---|
| |
| Role | Advanced trainer |
| National origin | Argentina |
| Manufacturer | Instituto Aerotécnico
|
| Designer | Ernesto Vicente |
| First flight | 1949 |
| Number built | 1 |
The I.Ae.32 Chingolo (named after
five year plan
.
Design and development
The design, which shared some of the technical characteristics of the earlier I.Ae. 31 Colibrí, was a conventional low-wing cantilever monoplane with and had fixed tailwheel undercarriage; seating a student pilot (or passenger) and instructor (or pilot) in a tandem enclosed cockpit. Only one prototype was built.
Specifications
General characteristics
- Crew: two, student pilot and instructor
- Length: 8.12 m (26 ft 8 in)
- Wingspan: 10.70 m (35 ft 1 in)
- Height: 2.10 m (6 ft 11 in)
- Wing area: 16.50 m2 (177.6 sq ft)
- Empty weight: 750 kg (1,653 lb)
- Gross weight: 981 kg (2,163 lb)
- Powerplant: 1 × Blackburn Cirrus Major 3 , 115 kW (155 hp)
Performance
- Maximum speed: 230 km/h (143 mph, 124 kn)
- Endurance: 1 hours 50 minutes
- Service ceiling: 5,180 m (16,990 ft)
See also
References
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 524.
- Bridgeman, Leonard. Jane's All The World's Aircraft 1950-1951 edition New York: The Mcgraw. Hill Book Company, Inc, 1950 Pg.9c (No ISBN)
Further reading
- Burzaco, Ricardo (1995). Las Alas de Perón, Aeronáutica Argentina 1945/1960 (in Spanish) (1st ed.). Buenos Aires: Editorial Da Vinci. ISBN 978-987-96764-4-8.
External links
Wikimedia Commons has media related to I.Ae. 32 Chingolo.